AXIOM-4, 64593 (Decayed)
Orbit data source: Space-Track
AXIOM-4, 64593 was a payload satellite owned by SpaceX (US) in LEO that was launched on Wed, 25 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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64593 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed Commercial Spaceship
Bus & Motor
DRAGON CM, Unknown motor
Mass
~13,000 kg wet, ~9,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trunc Cone + Cyl + 4 Fin, 14.5 m
Radar Cross Section
21.677 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 AXIOM-4
1 64593U 25136A 25195.85349944 .00004183 00000-0 10000-3 0 9992
2 64593 51.6363 169.9496 0003692 8.7454 351.3140 15.43789036 3045Epoch: 2025-07-14T20:29Z
TLE epoch observation values (Epoch: 2025-07-14T20:29:02.351Z)
Latitude
-0.03602°
Longitude
-70.29496°
Altitude
433.196 km
Speed
7.654 km/s
True Right ascension
11h 19m 41s
True Declination
0° 02' 09"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.961 km
Perigee altitude
432.93 km
Semi-major axis
6,813.583 km
Eccentricity
0.00037
Inclination
51.6363°
RAAN
169.9496°
Arg. of periapsis
8.7454°
True anomaly
351.30761°
Mean anomaly
351.314°
Eccentric anomaly
351.3108°
Mean motion
3.85905 °/min
Orbital period
93.29 mins
BSTAR
0.0001
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Other satellites on launch #136 in the year 2025 (2025-06-25 UTC)
No other RSOs were in this launch
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.AXIOM-4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 10:03:34.075Z | 183.906° SSW | 2026-06-21 10:05:34.075Z | 141.989° SSE | 22.129° | 2026-06-21 10:08:34.075Z | 78.009° E |
| 5 mins | 2026-06-21 11:40:34.075Z | 268.25° W | 2026-06-21 11:42:34.075Z | 324.942° NNW | 31.665° | 2026-06-21 11:45:34.075Z | 38.281° NE |
| 4 mins | 2026-06-21 16:34:34.075Z | 339.696° N | 2026-06-21 16:36:34.075Z | 47.829° ENE | 28.212° | 2026-06-21 16:38:34.075Z | 91.211° ESE |
| 4 mins | 2026-06-21 18:11:34.075Z | 266.559° W | 2026-06-21 18:12:34.075Z | 239.995° WSW | 24.469° | 2026-06-21 18:15:34.075Z | 168.089° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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